Wind Measurement Method without Aerodynamics Angles of Attack and Sideslip for Small Unmanned Aircraft Vehicle

被引:0
|
作者
Zhou Wei-jing [1 ]
Li Yi-yong [1 ]
Shen Huai-rong
机构
[1] Acad Equipment Command & Technol, Co Postgrad Management, Beijing 101416, Peoples R China
关键词
wind measurement; unmanned aircraft vehicle; angle of attack; angle of sideslip; pitot tube;
D O I
暂无
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
A new approach for on-board determination of the wind speed and direction for small unmanned aircraft vehicle is presented. Using the data from the airspeed system (a nose-mounted pitot tube and temperature sensors) and with the coordinate transformation matrix from the attitude determination system, the air speed vector in the geodetic coordinate system can be obtained by establishing equations. Then, together with the velocity of the aircraft from the aircraft navigation system (GPS), it is possible to estimate the wind vector without angles of attack and sideslip and to achieve the low-cost and convenient goal. Results from simulations are presented for verification of the wind measurement method.
引用
收藏
页码:171 / 174
页数:4
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